Scott D. Lewis
41Patents
4h-index
31Co-inventors
55Inventor score
Filing activity: May 31, 2012 → Aug 27, 2020
Most-cited inventions
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US9284845B2 | Turbine airfoil tip shelf and squealer pocket cooling | Emerging Cross-Sectional Technologies | 14 | Active |
| US8584470B2 | Tri-lobed cooling hole and method of manufacture | Emerging Cross-Sectional Technologies | 11 | Active |
| US10677066B2 | Turbine blade with airfoil tip vortex control | Emerging Cross-Sectional Technologies | 7 | Active |
| US10100645B2 | Trailing edge cooling configuration for a gas turbine engine airfoil | Emerging Cross-Sectional Technologies | 5 | Active |
| US10208603B2 | Staggered crossovers for airfoils | Emerging Cross-Sectional Technologies | 3 | Active |
| US10145246B2 | Staggered crossovers for airfoils | Emerging Cross-Sectional Technologies | 3 | Active |
| US11029027B2 | Dilution/effusion hole pattern for thick combustor panels | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10773344B2 | Systems and methods for manufacturing film cooling hole diffuser portion | Mechanical Engineering; Lighting; Heating | 3 | Active |
| US10801325B2 | Turbine blade with tip vortex control and tip shelf | Emerging Cross-Sectional Technologies | 3 | Active |
| US9822658B2 | Grooved seal arrangement for turbine engine | Emerging Cross-Sectional Technologies | 3 | Active |
| US10156144B2 | Turbine airfoil and method of cooling | Emerging Cross-Sectional Technologies | 3 | Active |
| US10502066B2 | Turbine engine component including an axially aligned skin core passage interrupted by a pedestal | Emerging Cross-Sectional Technologies | 2 | Active |
| US11168570B1 | Cooling arrangement for gas turbine engine components | Emerging Cross-Sectional Technologies | 2 | Active |
| US10180067B2 | Mate face cooling holes for gas turbine engine component | Mechanical Engineering; Lighting; Heating | 2 | Active |
| US10422230B2 | Cooling hole with curved metering section | Emerging Cross-Sectional Technologies | 2 | Active |
| US9243500B2 | Turbine blade platform with U-channel cooling holes | Emerging Cross-Sectional Technologies | 2 | Active |
| US10041356B2 | Showerhead hole scheme apparatus and system | Emerging Cross-Sectional Technologies | 2 | Active |
| US10077667B2 | Turbine airfoil film cooling holes | Emerging Cross-Sectional Technologies | 2 | Active |
| US11352902B2 | Cooling arrangement including alternating pedestals for gas turbine engine components | Emerging Cross-Sectional Technologies | 1 | Active |
| US10053992B2 | Gas turbine engine airfoil squealer pocket cooling hole configuration | Emerging Cross-Sectional Technologies | 1 | Active |
| US10392943B2 | Film cooling hole including offset diffuser portion | Emerging Cross-Sectional Technologies | 1 | Active |
| US10408071B2 | BOAS thermal protection | Emerging Cross-Sectional Technologies | 1 | Active |
| US9982542B2 | Airfoil platform impingement cooling holes | Emerging Cross-Sectional Technologies | 1 | Active |
| US10227875B2 | Gas turbine engine component with combined mate face and platform cooling | Emerging Cross-Sectional Technologies | 1 | Active |
| US10323524B2 | Axial skin core cooling passage for a turbine engine component | Emerging Cross-Sectional Technologies | 1 | Active |
Source: USPTO / EPO open patent data. Inventor disambiguation is heuristic; counts are objective bibliographic measures.